Computation of viscous hypersonic flow over control surfaces
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Computation of supersonic turbulent flows over an inclined ogive-cylinder-flarePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical solution of supersonic laminar flow over an inclined body of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computation of the Viscous Supersonic Flow over External Axial CornersAIAA Journal, 1979
- A detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical simulation of supersonic and hypersonic turbulent compression corner flows using relaxation modelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner FlowsAIAA Journal, 1976